Unsteady effects on trailing edge cooling

Journal of Heat Transfer

Volumn 127, Issue 4, 2005, Pages 388-392

  Medic, G ^a   Durbin, P A ^a  

^a Stanford University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; HEAT TRANSFER; REYNOLDS NUMBER; TURBINES; TURBOMACHINE BLADES;

ADIABATIC EFFECTIVENESS; EDGE COOLING FLOWS; SURFACE JETS; TURBINE BLADES;

COOLING;

COOLING; HEAT TRANSFER; TURBINE;

EID: 18844426317     PISSN: 00221481     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1860565     Document Type: Article

References (6)

1. Holloway, S. D., Leylek, J. H,, and Buck, F. A., 2002, "Pressure-Side Bleed Film Cooling: Part I, Steady Framework for Experimental and Computational Results," ASME Turbo Expo 2002; papers GT-2002-30471.
2. Iaccarino, G., Ooi, A., Durbin, P. A., and Behnia, M., 2003, "Reynolds Averaged Simulation of Unsteady Separated Flow," Int. J. Heat Mass Transfer, 24, pp. 147-156.
3. Holloway, S. D., Leylek, J. H., and Buck, F. A., 2002, "Pressure-Side Bleed Film Cooling: Part 2, Unsteady Framework for Experimental and Computational Results," ASME Turbo Expo 2002, papers GT-2002-30472.
4. Rigby, D. L., and Bunker, R. S., 2002, "Heat Transfer in a Complex Trailing Edge Passage for a High Pressure Turbine Blade," NASA/CR 2002-211701.
5. Martini, P., and Shultz, A., 2004, "Experimental and Numerical Investigation of Trailing Edge Film Cooling by Circular Coolant Wall Jets Ejected From a Slot With Internal Rib Arrays," ASME J. Turbomach., 126, pp. 229-236.
6. Moser, M. M., and Rogers, R. D., 1991, "Mixing Transition in the Cascade to Small Scales in a Plane Mixing Layer," Phys. Fluids A, 3 , pp. 1128-1134.